US9827938B2ActiveUtilityA1

Apparatus, system, and method for diagnosing initiators in airbag systems

41
Assignee: TAKATA PROT SYSTEMS INCPriority: May 2, 2014Filed: Oct 17, 2016Granted: Nov 28, 2017
Est. expiryMay 2, 2034(~7.8 yrs left)· nominal 20-yr term from priority
B60R 2021/01184B60R 21/017B60R 21/01G07C 5/008G01R 31/006B60R 21/0173
41
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Claims

Abstract

The present invention discloses embodiments of an apparatus, system and related method for diagnosing initiators in air bag systems. An embodiment of the system comprises a diagnostic circuit electrically connected between acceleration switches and one or more squib, that is user-activated via a momentary switch, and with user-feedback, wherein a user can diagnose the health of the one or more squib with no power drain while inactive. An embodiment of a method related to the system comprises activating a momentary switch, completing a circuit whereby a diagnostic circuit may function, indicating to the user that the diagnostic circuit is functioning, regulating the current into the diagnostic circuit so that the squib does not fire, boosting the signal to a window comparator, detecting the desired voltage by the window comparator, giving feedback to the user that the voltage is good, too high, or too low. An apparatus embodiment of the present invention may comprise an electronics control module for sensing a crash event and initiating an inflation sequence for one or more airbags with an integrated system for diagnosing one or more initiators. The apparatus may include a housing enclosing one or more circuit boards, to which may be electrically connected one or more wire harnesses which themselves are electrically connected to one or more squibs.

Claims

exact text as granted — not AI-modified
What is claimed is: 
     
       1. A system for diagnosing a plurality initiators in aircraft airbag systems where the system is configured to diagnose a plurality of aircraft seats installed in an aircraft, the system comprising:
 a diagnostic circuit electrically connected between an aircraft crash sensing means and a plurality of connected aircraft airbag initiators, the diagnostic circuit being in a normally off condition and enabled by a user activation; 
 a power supply, independent of the aircraft power, electrically connected to the diagnostic circuit; and 
 a visual indicator to a user of the health of each of the plurality of initiators, said visual indicator configured to be operative once the user has activated the diagnostic circuit.

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